The mechanism of strengthening of fibre materials fabricated by self-adhesive bonding during aerodynamic spinning was investigated. The effect of the structural indexes on the breaking strength of copolyatnide, polypropylene, and pol),cunide fibre materials was assessed. A mixed mechanism of their failure was established. A correlation was found between the structural indexes and the technological parameters of aerodynamic spinning.In aerodynamic spinning of fibre materials from melts, high-temperature stretching of the jet takes place. The fibres formed are transported by air to the take-up device, where they are glued together by the residual heat in them, forming a fibre lap [I].We will use the results obtained in studying glued nonwoven materials to assess the effect of structural elements on the physicomechanical properties of fibre lap. The structure of glued nonwoven materials and the arbitrary separation of these materials as a function of the degree of gluing into weakly, moderately, and strongly glued were qualitatively evaluated based on an znalysis of the deformation curves in [2]. It was hypothesized in [ 1,[3][4][5] that the least strong structural elements break more frequently in real fibre materials: the adhesive joints in weakly glued materials and the fibres in strongly glued materials.At the same time, a mixed mechanism of fracture of the materials was also hypothesized. In this case, both fibres and adhesive joints fracture. These hypotheses are based on the results of a study of models of nonwoven materials constructed from wires [4] with different elastic properties than the polymer fibres and on elementary models consisting of several glued fibres simulating glued nonwoven materials [6].The results of the study suggest the existence of two main ways of increasing the strength of fibre materials: due to an increase in the number of adhesive joints in the lap with a simultaneous decrease in the distance between them, or due to an increase in the strength of the individual adhesive joint with simultaneous preservation of a sufficient distance (300-400 lain) between adhesive joints. It should be noted that the strength of fibre materials fabricated by high-temperature stretching of polymer jets with subsequent thermal bonding is a function of the spinning conditions [2] and factors related to the structure of the fibre lap. The mechanism of strengthening differs significantly from the mechanism of the strength of materials fabricated by aerodynamic spinning of "cold" fibres not glued in the lap, which we investigated in detail in [8].The mechanism of strengthening of polymeric fibre materials fabricated by self-adhesive bonding during aerodynamic spinning is discussed in the present article. Model samples represented by fibre networks consisting of fibres of variable diameter from 50 to 400 pan were investigated in the first stage.The model samples were fabricated by gravity spinning on an OVN-I installation. Spinning and self-adhesive bonding of the fibres in the model materials was attained...